# N560AU: 1987 Boeing 737-301, registration cancelled 2007-03-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 8, 2007
- Status when cancelled: Valid registration
- Airframe: [Boeing 737-301](https://openairdocs.org/model/boeing-737-301) (registry code 138447R)
- Engine: [CFM International CFM56 series](https://openairdocs.org/engine/cfm-international-cfm56-series) (registry code 13802)
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) (OpenAirDocs)
- Serial number: 23514
- Year built: 1987
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: January 22, 1987
- Certificate issued: September 1, 2006
- Last registry action: September 1, 2006
- Mode S code: A726FD
- Owner when cancelled: [Jet Partners LLC](https://openairdocs.org/faa-owner/JET%20PARTNERS%20LLC)
- Location: [New York, NY](https://openairdocs.org/faa-place/NY/New%20York)
- Owner type: Corporation
- Owner's area on the map: 40.7657° N, 73.9851° W: Placed by OpenAirDocs at the center of ZIP code 10019, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N560AU
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=560AU
- Page: https://openairdocs.org/deregistered/N560AU-2007-03-08

From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 737-301: https://openairdocs.org/model/boeing-737-301.md

## Service difficulty reports (70, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR USAA050589](https://openairdocs.org/sdr/USAA050589), May 3, 2005: STIFFENER. CRACKED. CLT - FOUND STIFFENER CRACKED .4 INCH IN VERTICAL STIFFENER AT AFT SIDE OF PYLON LOWER SIDE OF WING. FABRICATED REPAIR PART AND INSTALLED SRM 51-10-02. (M)
- [SDR USAASB04010](https://openairdocs.org/sdr/USAASB04010), Jan 21, 2004: CHARGER. INOPERATIVE. PHL - MAINTENANCE REPORTED THE RIGHT OVERWING EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER ASSEMBLY. OPS CHECK GOOD. (M
- [SDR USAASB03221](https://openairdocs.org/sdr/USAASB03221), Dec 24, 2003: FUSE. INOPERATIVE. DCA- MAINTENANCE REPORTED THE EMERGENCY ESCAPE PATH SEAT MOUNTED LIGHTS ON SEAT ROWS 6, 7, 8, 9 AND 11 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A BLOWN FUS
- [SDR USAA030194](https://openairdocs.org/sdr/USAA030194), Sep 10, 2003: SKIN. CRACKED. FOUND SKIN CRACKED 2.250 INCH, JUST BELOW S23R AT FS 730. INSTALLED DOUBLER/TRIPLER PER SRM 53-00-01, FIG 229, PROCEDURE V, DETAIL IV. (M)
- [SDR USAA030193](https://openairdocs.org/sdr/USAA030193), Sep 10, 2003: SKIN. CRACKED. FOUND SKIN CRACKED .750 INCH, FUSELAGE JUST ABOVE S24R FORWARD OF FS 727E. INSTALLED DOUBLR/TRIPLER PER SRM 53-00-01, FIG 229, PROCEDURE V, DETAIL IV. (M)
- [SDR USAA030187](https://openairdocs.org/sdr/USAA030187), Sep 8, 2003: SKIN. CRACKED. CLT - FOUND SKIN CRACKED 2.5 INCHES, FUSELAGE SKIN JUST BELOW S19R AT FS 760. INSTALLED DOUBLER PER SRM 53-00-01, FIG 229. (M)
- [SDR USAA030117](https://openairdocs.org/sdr/USAA030117), Jul 17, 2003: SKIN. DAMAGED. PIT - FOUND RUDDER WITH SKIN DAMAGE, 24 INCH OVAL ONE LAYER DAMAGE, LEFT SIDE OF RUDDER 107 INCH FROM BOTTOM 12 INCHES FROM TRAILING EDGE. WET LAY UP REPAIR PER
- [SDR USAA030119](https://openairdocs.org/sdr/USAA030119), Jul 17, 2003: FLOORBEAM. CRACKED. PIT - FOUND FLOORBEAM CRACKED APPROX 1 INCH, BS 328 RBL 10.0. DOUBLER INSTALLED PER EA 76205. (M)
- [SDR USAA030118](https://openairdocs.org/sdr/USAA030118), Jul 11, 2003: ANGLE. CRACKED. PIT - FOUND ANGLE HAS .375 INCH CRACK, NR 5 LE SLAT ACTUATOR ATTACH FITTING ANGLE. FABRICATED REPAIR ANGLE FROM 17-7 PH PER EA 76202. (M)
- [SDR USAA030116](https://openairdocs.org/sdr/USAA030116), Jul 8, 2003: SUPPORT FITTING. CRACKED. PIT - FOUND MLG BEAM AFT SUPPORT FITTING HAS APPROX .5 INCH CRACK, UPPER OUTBOARD HOLD ON MLG BEAM AFT SUPPORT FITTING, RSS 224.14. OVERSIZED HOLE AND INSTALLED
- [SDR USAA030089](https://openairdocs.org/sdr/USAA030089), May 22, 2003: FLOORBEAM. CORRODED. PIT - FOUND FLOORBEAM CORRODED APPROX 6 INCHES BY 1 INCH, FLOORBEAM BETWEEN STATION 344 AND 360 10 INCHES LBBL. MANUFACTURED AND INSTALLED T-CAP PER EA 76223 SR
- [SDR USAA030060](https://openairdocs.org/sdr/USAA030060), May 22, 2003: BELTFRAME. CRACKED. PIT - FOUND BELTFRAME CRACKED .1875 INCH, BELTFRAME CRACKED AT STATION 303.9 STRINGER 13L. DOUBLER INSTALLED PER EA 76233. (M)
- [SDR USAA030079](https://openairdocs.org/sdr/USAA030079), May 22, 2003: ANGLE. CRACKED. PIT - FOUND RUDDER CRACKED .5 INCH, RUDDER LOWER FORWARD SEAL PLATE ANGLE. INSTALLED WET LAYUP REPAIR PER EA 76293, SRM 51-70-17 AND 51-60-00. (M)
- [SDR USAA030050](https://openairdocs.org/sdr/USAA030050), May 6, 2003: SKIN. CORRODED. FOUND SKIN CORRODED 1 INCH AREA AND .5 INCH AREA, AROUND FASTENER, BL 0 STATION 1016 RADIAL STIFFENER. CORROSION LEVEL 1. REMOVED DAMAGED END OF STIFFENER, INST
- [SDR USAA030083](https://openairdocs.org/sdr/USAA030083), May 5, 2003: BEAR STRAP. CRACKED. FOUND BEAR STRAP CRACKED .1875 INCH, MED BEAR STRAP BS 304 UPPER AND LOEWR HINGE CUTOUT. INSTALLED DOUBLERS PER EA 76233. (M)
- [SDR USAA030147](https://openairdocs.org/sdr/USAA030147), May 1, 2003: NUT PLATE. CORRODED. PIT - FOUND NUTPLATE CORRODED .75 INCH BY 1 INCH AREA, FS 727A-727B 21 LT. INSTALLED DOUBLER PER SRM 53-00-3. CORROSION LEVEL 1, TASK NR C53-107-01. (M)
- [SDR USAA030096](https://openairdocs.org/sdr/USAA030096), Apr 30, 2003: BELTFRAME. CRACKED. PIT - FOUND BELTFRAME CRACKED .75 INCH LONG, AT RIVET FOR LOWER OVERHEAD BIN, BETWEEN S8L AND S9L, FS 440. PER TYPICAL REPAIR PER 53-10-20A. (M)
- [SDR USAA030082](https://openairdocs.org/sdr/USAA030082), Apr 27, 2003: FRAME. CRACKED. PIT - FOUND FRAME CRACKED .1875 INCH, SMALL CRACK IN FRAME AT RIVET STATION 360 LEFT, BETWEEN 58-59. REMOVED DAMAGED AND INSTALLED DOUBLERS PER TR 53-10-20A. (M
- [SDR USAA030059](https://openairdocs.org/sdr/USAA030059), Apr 25, 2003: FITTING. CRACKED. FOUND FITTING CRACKED 1.5 INCHES LONG, FITTING IN HORIZONTAL STABILIZER CENTER SECTION OF RIGHT THRUST BEAM. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)
- [SDR USAA020177](https://openairdocs.org/sdr/USAA020177), Apr 16, 2002: SKIN. CRACKED. PIT - FOUND SKIN AND WEB PLATE CRACKED .625 INCH, BS 360-380, AT BL 10. SKIN DOUBLER ADDED PER TYPICAL REPAIR 53-30-07 AND EA 73800. (M)
- [SDR USAASB01346](https://openairdocs.org/sdr/USAASB01346), Dec 20, 2001: LIGHT. INOPERATIVE. CLT - PILOT REPORTED THE FLOOR PATH EMERGENCY LIGHTING, AT SEAT ROW 13C, IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEM
- [SDR USAASB99278](https://openairdocs.org/sdr/USAASB99278), Nov 25, 1999: INDICATOR. FAILED. CLT - FLT 2202 - DURING CLIMB-OUT FROM CLT, THE FLAPS FAILED TO RETRACT AS FLAP INDICATOR FAILED AT 5 DEGREES FLAPS. FLIGHT RETURNED TO FIELD AT CLT AND LANDED 
- [SDR USAA991218](https://openairdocs.org/sdr/USAA991218), Nov 11, 1999: ANTENNA BASE. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 12 INCH AREA OF CORROSION BETWEEN STRINGER 28 LT AND RT AFT OF STATION 500 ANTENNA BASE, CORROSION L
- [SDR USAA991215](https://openairdocs.org/sdr/USAA991215), Nov 11, 1999: SHEAR TIE. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 420 STRINGER 4 LEFT SHEAR TIE. REMOVED AND REPLACED PER SRM 51-10-2. (M)
- [SDR USAA991214](https://openairdocs.org/sdr/USAA991214), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 500 RIGHT STRINGER 15 SHEAR TIE DAMAGE AT STRINGER AND FRAME. REMOVED AND REPLACED PER 
- [SDR USAA991213](https://openairdocs.org/sdr/USAA991213), Nov 11, 1999: BULKHEAD. CRACKED. CLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 2 WEB. INSTALLED DOUBLER P
- [SDR USAA991212](https://openairdocs.org/sdr/USAA991212), Nov 11, 1999: BULKHEAD. CRACKED. CLT - DURING Q-2 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK 178 BULKHEAD 5 INCH BELOW FLOOR LEVEL AT STIFFENER NR 3 WEB. INSTALLED DOUBLER P
- [SDR USAA991211](https://openairdocs.org/sdr/USAA991211), Nov 11, 1999: SKIN. CRACKED. CLT - DURIGN Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK ON NR 2 ENGINE PYLON AT ACCESS PANEL NR 5824R UPPER FORWARD CORNER SKIN. INSTALLED DOUBLER PER EA
- [SDR USAA991210](https://openairdocs.org/sdr/USAA991210), Nov 11, 1999: ANGLE. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 10 INCH AREA OF CORROSION AT AFT ENTRY DOOR FLOOR Z-ANGLE, CORROSION LEVEL 1. REMOVED AND REPLACED Z
- [SDR USAA991208](https://openairdocs.org/sdr/USAA991208), Nov 11, 1999: T-CAP. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TEN 1 INCH BY 1 INCH AREAS OF CORROSION ON UPPER CAP OF T-CAP STATION 967, CORROSION LEVEL 2. REPLACED T-CAP PER
- [SDR USAA991207](https://openairdocs.org/sdr/USAA991207), Nov 11, 1999: ANGLE. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT AFT ENTRY DOOR Z-ANGLE (CHANNEL), CORROSION LEVEL 2, CORROSION TASK NR C53-107-02.
- [SDR USAA991206](https://openairdocs.org/sdr/USAA991206), Nov 11, 1999: ANGLE. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 20 INCH AREA OF CORROSION AT RT AFT SERVICE DOOR Z-ANGLE (FLOOR), CORROSION LEVEL 2, CORROSION TASK 
- [SDR USAA991205](https://openairdocs.org/sdr/USAA991205), Nov 11, 1999: SEAT TRACK. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 2 INCH AREA OF CORROSION AT BS 727B-947 SEAT TRACK, CORROSION LEVEL 2. INSTALLED SEAT TRACK PER SRM 
- [SDR USAA991204](https://openairdocs.org/sdr/USAA991204), Nov 11, 1999: FLOORBEAM. CORRODED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 1 INCH MULTIPLE AREA OF CORROSION AT BS 986.5, RBL 44 - LBL 45, FLOORBEAM T-CAP. CORROSION LEVEL 2. 
- [SDR USAA991198](https://openairdocs.org/sdr/USAA991198), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 908 STRINGER 9L BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND SRM 53-00-07. (M)
- [SDR USAA991197](https://openairdocs.org/sdr/USAA991197), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND SRM 53-00-07. (M)
- [SDR USAA991196](https://openairdocs.org/sdr/USAA991196), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT BS 867 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)
- [SDR USAA991195](https://openairdocs.org/sdr/USAA991195), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 827 STRINGER 9L BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)
- [SDR USAA991194](https://openairdocs.org/sdr/USAA991194), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1.2 5INCH CRACK AT BS 727D STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)
- [SDR USAA991193](https://openairdocs.org/sdr/USAA991193), Nov 11, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 663 STRINGER 10R TIE CLIP. REPLACED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA991192](https://openairdocs.org/sdr/USAA991192), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STRINGER 8 AND 9L FRAME. INSTALLED DOUBLER PER TR 53-10-14 AND EA 65950. (M)
- [SDR USAA991191](https://openairdocs.org/sdr/USAA991191), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT BS 727 STRINGER 14L OUTER CHORD ANGLE. REPAIRED DOUBLER AND TRIPLER PER EA 65952. (M)
- [SDR USAA991190](https://openairdocs.org/sdr/USAA991190), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK IN FUSE FRAME AT FASTENER HOLE BS 480 BETWEEN STRINGER 8 AND 9R. INSTALLED DOUBLER PER TR 53-
- [SDR USAA991189](https://openairdocs.org/sdr/USAA991189), Nov 11, 1999: BULKHEAD. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .250 INCH CRACKS IN 2 PLACES STATION 178 WEB A AND WEB B, LBL 1 AND RBL 1 SKIN. INSTALLED DOUBLER PER SRM 53-1
- [SDR USAA991188](https://openairdocs.org/sdr/USAA991188), Nov 11, 1999: SKIN. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND TWO 1 INCH CRACKS AT BS 663, LBL 32 CEILING PRESSURE DECK. INSTALLED DOUBLER PER TR 53-60-04 AND SRM 53-60-51. (
- [SDR USAA991187](https://openairdocs.org/sdr/USAA991187), Nov 11, 1999: SKIN. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AT RIGHT HORIZONTAL STABILIZER LOWER SURFACE STATION 111-166 SKIN. INSTALLED DOUBLER AND FILLER P
- [SDR USAA991186](https://openairdocs.org/sdr/USAA991186), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK THROUGH RIVET HOLE BS 847, STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER TR 53-10-14. (M)
- [SDR USAA991185](https://openairdocs.org/sdr/USAA991185), Nov 11, 1999: TIE CLIP. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND .250 INCH CRACK AT BS 727B STRINGER 4L TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-02. (M)
- [SDR USAA991184](https://openairdocs.org/sdr/USAA991184), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 807 STRINGER 9R BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)
- [SDR USAA991183](https://openairdocs.org/sdr/USAA991183), Nov 11, 1999: FRAME. CRACKED. CLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT RIVET BS 887 STRINGER 91 BELT FRAME. INSTALLED DOUBLER PER EA 65950 AND TR 53-10-14. (M)

All 70: https://openairdocs.org/deregistered/N560AU-2007-03-08/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19980714036349I](https://openairdocs.org/incident/19980714036349I), Jul 14, 1998: Boeing 737301 (N560AU), Pittsburgh, PA, Minor damage. Aircraft landed long on runway 32, ran off the end.

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